An aircraft (100) includes a body (10) and an outer frame (1) rotatably coupled to the body (10). The body (10) includes a plurality of rotary blades (15a-15d) and a driver (14a-14d) configured to rotate the plurality of rotary blades (15a-15d). The outer frame (1) includes a rotary frame (1a-1c) rotatable about a rotation axis intersecting the direction of gravity, and a center of gravity of the plurality of rotary blades (15a-15d) and the driver (14a-14d) is located lower than the rotation axis in the direction of gravity.
AIRCRAFT, FLIGHT SYSTEM, AND STRUCTURE INSPECTION SYSTEM
FLUGZEUG, FLUGSYSTEM UND STRUKTURINSPEKTIONSSYSTEM
AÉRONEF, SYSTÈME DE VOL ET SYSTÈME D'INSPECTION DE STRUCTURE
24.01.2024
Patent
Elektronische Ressource
Englisch
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